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SINS-CNS.rar
- 弹道导弹SINS/CNS组合导航的程序，在发射点惯性坐标系下,Ballistic Missile SINS/CNS Integrated Navigation of the program, the launch point inertial coordinate system
LabVIEW-basedsimulationoftheopenspacesystemdesignb
- 基于LabVIEW的空地导弹弹道仿真系统设计-LabVIEW-based simulation of the open space system design ballistic missile
Kepler_orbit_rotate
- 计算得出导弹的被动段飞行轨迹（未考虑大气）和再入点、落点信息（在发射惯性坐标系内的位置量）-Calculated the passive missile flight path segment (not to consider the atmosphere) and re-entry point, placement of information (in the firing position within the inertial coordinate system volume)
missle--control--design
- 导弹控制系统鲁棒设计程序源代码，可以用来参考编程，比较实用-missile control system design
gas-and-steam-launch
- 水下潜艇导弹燃气蒸汽式弹射时的内弹道方程和参数求解。-Solving interior ballistic equations and parameters when missile launched by gas and steam system on submarine.